Invention Application
- Patent Title: THRUST REVERSER COMPRISING FIXED CASCADES AND A SEALING MEMBRANE
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Application No.: US18726915Application Date: 2023-01-06
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Publication No.: US20250101931A1Publication Date: 2025-03-27
- Inventor: Patrick GONIDEC , Loïc CHAPELAIN (Deceased) , Patrick André BOILEAU
- Applicant: SAFRAN NACELLES
- Applicant Address: FR Gonfreville-L'Orcher
- Assignee: SAFRAN NACELLES
- Current Assignee: SAFRAN NACELLES
- Current Assignee Address: FR Gonfreville-L'Orcher
- Priority: FR2200134 20220110
- International Application: PCT/FR2023/050014 WO 20230106
- Main IPC: F02K1/72
- IPC: F02K1/72

Abstract:
A thrust reverser for an aircraft propulsion assembly, including a fixed structure equipped with at least one cascade as well as a radially inner delimiting wall of a secondary vein, and a movable structure including at least one reverser cowling, the cascade being arranged, in the forward direct thrust position, in a housing of the reverser cowling, and, in the retracted thrust reversal position, the wall reveals a passage opening of the secondary vein towards the cascade, the thrust reverser also including at least one sealing membrane designed to deflect at least one portion of the secondary flow. A hook is provided for securing the membrane to a rear cascade support frame, and to the radially inner delimiting wall of the secondary vein.
Information query
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